RADOME FOR AVIATION BODY AND MANUFACTURING METHOD OF THE SAME
PROBLEM TO BE SOLVED: To provide a radome for an aviation body, light weight, having a sandwich structure of a three-dimensional shape, excellent in electromagnetic wave transmissivity and a manufacturing method of the same.SOLUTION: The radome for an aviation body has a shape of covering an electro...
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| creator | KUME MASASANE KOBAYASHI HIROKI |
| description | PROBLEM TO BE SOLVED: To provide a radome for an aviation body, light weight, having a sandwich structure of a three-dimensional shape, excellent in electromagnetic wave transmissivity and a manufacturing method of the same.SOLUTION: The radome for an aviation body has a shape of covering an electromagnetic wave instrument installed on an aviation body, and is formed with a sandwich panel structure in which a core material (30), compounded by foaming insulting reinforced fiber (31) and a heat-resistant resin (32), is held between skin materials (20), composed of a fiber-reinforced material formed by compounding a quartz cloth (21) and a heat-resistant resin (22).SELECTED DRAWING: Figure 1
【課題】軽量で電波透過性の優れた３次元形状のサンドイッチ構造を有する飛行体用レドームおよび飛行体用レドームの製造方法を得る。【解決手段】本発明に係る飛行体用レドームは、飛行体に搭載されている電波機器を覆う形状を有しており、石英クロス（２１）と耐熱性樹脂（２２）とが複合化された繊維強化材からなるスキン材（２０）の間に、絶縁性の強化繊維（３１）と、耐熱性樹脂（３２）とを発泡させて複合化させたコア材（３０）を挟んだサンドイッチパネル構造により形成されている。【選択図】図１ |
| format | Patent |
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【課題】軽量で電波透過性の優れた３次元形状のサンドイッチ構造を有する飛行体用レドームおよび飛行体用レドームの製造方法を得る。【解決手段】本発明に係る飛行体用レドームは、飛行体に搭載されている電波機器を覆う形状を有しており、石英クロス（２１）と耐熱性樹脂（２２）とが複合化された繊維強化材からなるスキン材（２０）の間に、絶縁性の強化繊維（３１）と、耐熱性樹脂（３２）とを発泡させて複合化させたコア材（３０）を挟んだサンドイッチパネル構造により形成されている。【選択図】図１</description><language>eng ; jpn</language><subject>AEROPLANES ; AIRCRAFT ; ANTENNAS, i.e. RADIO AERIALS ; AVIATION ; BASIC ELECTRIC ELEMENTS ; COSMONAUTICS ; ELECTRICITY ; HELICOPTERS ; LAYERED PRODUCTS ; LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2016</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160818&DB=EPODOC&CC=JP&NR=2016149756A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160818&DB=EPODOC&CC=JP&NR=2016149756A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KUME MASASANE</creatorcontrib><creatorcontrib>KOBAYASHI HIROKI</creatorcontrib><title>RADOME FOR AVIATION BODY AND MANUFACTURING METHOD OF THE SAME</title><description>PROBLEM TO BE SOLVED: To provide a radome for an aviation body, light weight, having a sandwich structure of a three-dimensional shape, excellent in electromagnetic wave transmissivity and a manufacturing method of the same.SOLUTION: The radome for an aviation body has a shape of covering an electromagnetic wave instrument installed on an aviation body, and is formed with a sandwich panel structure in which a core material (30), compounded by foaming insulting reinforced fiber (31) and a heat-resistant resin (32), is held between skin materials (20), composed of a fiber-reinforced material formed by compounding a quartz cloth (21) and a heat-resistant resin (22).SELECTED DRAWING: Figure 1
【課題】軽量で電波透過性の優れた３次元形状のサンドイッチ構造を有する飛行体用レドームおよび飛行体用レドームの製造方法を得る。【解決手段】本発明に係る飛行体用レドームは、飛行体に搭載されている電波機器を覆う形状を有しており、石英クロス（２１）と耐熱性樹脂（２２）とが複合化された繊維強化材からなるスキン材（２０）の間に、絶縁性の強化繊維（３１）と、耐熱性樹脂（３２）とを発泡させて複合化させたコア材（３０）を挟んだサンドイッチパネル構造により形成されている。【選択図】図１</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ANTENNAS, i.e. RADIO AERIALS</subject><subject>AVIATION</subject><subject>BASIC ELECTRIC ELEMENTS</subject><subject>COSMONAUTICS</subject><subject>ELECTRICITY</subject><subject>HELICOPTERS</subject><subject>LAYERED PRODUCTS</subject><subject>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLANcnTx93VVcPMPUnAM83QM8fT3U3Dyd4lUcPRzUfB19At1c3QOCQ3y9HNX8HUN8fB3UfB3UwjxcFUIdvR15WFgTUvMKU7lhdLcDEpuriHOHrqpBfnxqcUFicmpeakl8V4BRgaGZoYmluamZo7GRCkCAFbqKfY</recordid><startdate>20160818</startdate><enddate>20160818</enddate><creator>KUME MASASANE</creator><creator>KOBAYASHI HIROKI</creator><scope>EVB</scope></search><sort><creationdate>20160818</creationdate><title>RADOME FOR AVIATION BODY AND MANUFACTURING METHOD OF THE SAME</title><author>KUME MASASANE ; KOBAYASHI HIROKI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2016149756A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; jpn</language><creationdate>2016</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ANTENNAS, i.e. RADIO AERIALS</topic><topic>AVIATION</topic><topic>BASIC ELECTRIC ELEMENTS</topic><topic>COSMONAUTICS</topic><topic>ELECTRICITY</topic><topic>HELICOPTERS</topic><topic>LAYERED PRODUCTS</topic><topic>LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>KUME MASASANE</creatorcontrib><creatorcontrib>KOBAYASHI HIROKI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>KUME MASASANE</au><au>KOBAYASHI HIROKI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>RADOME FOR AVIATION BODY AND MANUFACTURING METHOD OF THE SAME</title><date>2016-08-18</date><risdate>2016</risdate><abstract>PROBLEM TO BE SOLVED: To provide a radome for an aviation body, light weight, having a sandwich structure of a three-dimensional shape, excellent in electromagnetic wave transmissivity and a manufacturing method of the same.SOLUTION: The radome for an aviation body has a shape of covering an electromagnetic wave instrument installed on an aviation body, and is formed with a sandwich panel structure in which a core material (30), compounded by foaming insulting reinforced fiber (31) and a heat-resistant resin (32), is held between skin materials (20), composed of a fiber-reinforced material formed by compounding a quartz cloth (21) and a heat-resistant resin (22).SELECTED DRAWING: Figure 1
【課題】軽量で電波透過性の優れた３次元形状のサンドイッチ構造を有する飛行体用レドームおよび飛行体用レドームの製造方法を得る。【解決手段】本発明に係る飛行体用レドームは、飛行体に搭載されている電波機器を覆う形状を有しており、石英クロス（２１）と耐熱性樹脂（２２）とが複合化された繊維強化材からなるスキン材（２０）の間に、絶縁性の強化繊維（３１）と、耐熱性樹脂（３２）とを発泡させて複合化させたコア材（３０）を挟んだサンドイッチパネル構造により形成されている。【選択図】図１</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT ANTENNAS, i.e. RADIO AERIALS AVIATION BASIC ELECTRIC ELEMENTS COSMONAUTICS ELECTRICITY HELICOPTERS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM PERFORMING OPERATIONS TRANSPORTING |
| title | RADOME FOR AVIATION BODY AND MANUFACTURING METHOD OF THE SAME |
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